CN112313147A - 飞行器减阻系统和内部冷却电动马达系统及使用它们的飞行器 - Google Patents

飞行器减阻系统和内部冷却电动马达系统及使用它们的飞行器 Download PDF

Info

Publication number
CN112313147A
CN112313147A CN201980032466.0A CN201980032466A CN112313147A CN 112313147 A CN112313147 A CN 112313147A CN 201980032466 A CN201980032466 A CN 201980032466A CN 112313147 A CN112313147 A CN 112313147A
Authority
CN
China
Prior art keywords
aircraft
nacelle
air
rotor
motor
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201980032466.0A
Other languages
English (en)
Chinese (zh)
Inventor
乔本·贝维尔特
格雷戈尔·维布勒·米基奇
乔伊·米利亚
罗布·托达尔
维什努·维图拉
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Geoby Flight Ltd
Original Assignee
Geoby Flight Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Geoby Flight Ltd filed Critical Geoby Flight Ltd
Publication of CN112313147A publication Critical patent/CN112313147A/zh
Pending legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/24Aircraft characterised by the type or position of power plants using steam or spring force
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/38Constructions adapted to reduce effects of aerodynamic or other external heating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C23/00Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/005Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/026Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings, or cowlings
    • B64D29/02Power-plant nacelles, fairings, or cowlings associated with wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/08Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C21/00Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/08Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like adjustable
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C2230/00Boundary layer controls
    • B64C2230/04Boundary layer controls by actively generating fluid flow
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0226Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising boundary layer control means

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Wind Motors (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Motor Or Generator Cooling System (AREA)
CN201980032466.0A 2018-03-16 2019-03-16 飞行器减阻系统和内部冷却电动马达系统及使用它们的飞行器 Pending CN112313147A (zh)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US201862643763P 2018-03-16 2018-03-16
US62/643,763 2018-03-16
US201862694910P 2018-07-06 2018-07-06
US62/694,910 2018-07-06
PCT/US2019/022651 WO2020033010A2 (en) 2018-03-16 2019-03-16 Aircraft drag reduction system and internally cooled electric motor system and aircraft using same

Publications (1)

Publication Number Publication Date
CN112313147A true CN112313147A (zh) 2021-02-02

Family

ID=68290934

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201980032466.0A Pending CN112313147A (zh) 2018-03-16 2019-03-16 飞行器减阻系统和内部冷却电动马达系统及使用它们的飞行器

Country Status (5)

Country Link
US (3) US11161589B2 (de)
EP (1) EP3765361A4 (de)
JP (2) JP7333144B2 (de)
CN (1) CN112313147A (de)
WO (1) WO2020033010A2 (de)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10900990B2 (en) * 2019-03-21 2021-01-26 Rosemount Aerospace Inc. Acoustic air data sensing systems with skin friction sensors
GB2587670A (en) * 2019-10-02 2021-04-07 Advanced Mobility Res And Development Ltd Systems and methods for aircraft
WO2021112940A1 (en) * 2019-12-04 2021-06-10 Beta Air, Llc An integrated electric propulsion assembly
US11613368B2 (en) * 2020-01-28 2023-03-28 Rolls-Royce Corporation Aircraft with electrical energy storage in nacelles
WO2021157736A1 (en) * 2020-02-06 2021-08-12 Hapsmobile Inc. Aerodynamic electric motor nacelle
US20230074332A1 (en) * 2020-02-21 2023-03-09 Eaton Intelligent Power Limited Integrated electric motor and thermal management system
US11472544B2 (en) * 2020-03-04 2022-10-18 Textron Innovations Inc. Electric drive system line replaceable unit with integrated collective actuation
US11565803B2 (en) 2020-03-04 2023-01-31 Textron Innovations Inc. Electric drive system line replaceable unit with integrated cyclic actuation
CN111348062A (zh) * 2020-03-21 2020-06-30 东莞理工学院 流体中高速移动物体降低阻力结构
US11831220B2 (en) 2020-06-22 2023-11-28 Textron Innovations Inc. Electric motor stack with integral one-piece gearbox input shaft
US11390395B2 (en) * 2020-06-25 2022-07-19 Textron Innovations Inc. Aircraft rotor assembly with segmented input shaft for electric motor stack and gearbox unit
US11781544B2 (en) * 2020-10-20 2023-10-10 Textron Innovations Inc. Electric drive system for rotorcraft
WO2022133486A1 (en) 2020-12-18 2022-06-23 Joby Aero, Inc. Electric motor comprising a liquid cooling of wound stator
US11814163B2 (en) 2021-01-13 2023-11-14 Textron Innovations Inc. Electric tiltrotor aircraft with tilting coaxial motors and gearbox
JP2024506334A (ja) * 2021-02-09 2024-02-13 ジョビー エアロ,インコーポレイテッド 航空機推進ユニット
WO2023041928A1 (en) * 2021-09-16 2023-03-23 Qdot Technology Ltd Integrated fan and battery propulsion system
CN114194403B (zh) * 2022-01-25 2023-06-02 广东汇天航空航天科技有限公司 驱动装置的散热结构及飞行器
EP4253251A1 (de) * 2022-03-28 2023-10-04 Lilium eAircraft GmbH Elektrisch angetriebene antriebseinheit eines luftfahrzeuges, luftfahrzeug und steuerverfahren für eine elektrisch angetriebene antriebseinheit
KR102613732B1 (ko) * 2022-05-30 2023-12-14 주식회사 플라나 열교환기 및 이를 포함하는 비행기
US11679872B1 (en) * 2022-12-12 2023-06-20 Archer Aviation Inc. Tilter motor cooling apparatus for vertical takeoff and landing aircraft and operating method of the same

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63289229A (ja) * 1987-05-06 1988-11-25 エムテーウー・モートレン‐ウント・ツルビーネン‐ウニオン・ミュンヘン・ゲーエムベーハー プロップ・ファン・ターボ駆動装置
US20130265848A1 (en) * 2010-06-01 2013-10-10 Esg Mbh Duct having flow conducting surfaces
WO2015004370A1 (fr) * 2013-07-12 2015-01-15 Hutchinson Dispositif de sustentation à soufflante(s) axiale(s), et aerodyne equipé d'un tel dispositif
EP2913269A1 (de) * 2014-02-28 2015-09-02 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Drehflügler mit mindestens einem Hauptrotor und mindestens einem Rotor zum Drehmomentausgleich
US9701399B1 (en) * 2013-03-18 2017-07-11 Techdyne Llc Parasitic drag induced boundary layer reduction system and method

Family Cites Families (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3128964A (en) * 1964-04-14 figures
US2620122A (en) 1945-10-09 1952-12-02 Herman H Curry Combination propeller and diffuser inlet assembly
US3262659A (en) * 1964-04-29 1966-07-26 John E Copeland Thrust control apparatus
US4397431A (en) * 1981-11-02 1983-08-09 Avco Corporation Fail-safe, anti-icing system for aircraft engines
US4456458A (en) * 1982-09-20 1984-06-26 The De Havilland Aircraft Of Canada, Limited Air intake system for engine
US4617028A (en) * 1983-11-03 1986-10-14 General Electric Company Aircraft engine air intake including a foreign object separator
US4607657A (en) * 1985-10-28 1986-08-26 General Electric Company Aircraft engine inlet
GB2196390B (en) * 1986-10-16 1991-06-26 Rolls Royce Plc Intake for turbopropeller gas turbine engine.
GB2203801B (en) * 1987-04-14 1991-11-27 Rolls Royce Plc A gas turbine engine
US5535967A (en) * 1993-12-20 1996-07-16 Alliedsignal Inc. Floating speed electrically driven suction system
US5725180A (en) * 1995-12-29 1998-03-10 General Electric Company Aircraft engine pitot plenum intake
US6041589A (en) * 1998-01-09 2000-03-28 General Electric Company Asymmetric turboprop booster
US6390418B1 (en) * 1999-02-25 2002-05-21 United Technologies Corporation Tangentially directed acoustic jet controlling boundary layer
US6761034B2 (en) * 2000-12-08 2004-07-13 General Electroc Company Structural cover for gas turbine engine bolted flanges
US6591873B1 (en) * 2001-11-21 2003-07-15 Air Cruisers Company Turbo fan aspirator
DE10162238A1 (de) 2001-12-18 2003-07-10 Rolls Royce Deutschland Lufteinlasssystem eines PTL-Antriebs
GB0313456D0 (en) * 2003-06-11 2003-07-16 Rolls Royce Plc Propulsion arrangement
DE602004032186D1 (de) 2004-12-01 2011-05-19 United Technologies Corp Turbinenschaufelgruppe eines Fanrotors sowie Verfahren zur Montage einer solchen Gruppe
WO2006116072A1 (en) 2005-04-21 2006-11-02 Syracuse University Cross-flow fan propulsion system
EP2143943A1 (de) * 2008-07-09 2010-01-13 Greenergy India Private Limited Windturbine
JP4856257B2 (ja) 2010-03-24 2012-01-18 川崎重工業株式会社 タービンロータのシール構造
US9227719B2 (en) * 2011-03-11 2016-01-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Reactive orthotropic lattice diffuser for noise reduction
US8464511B1 (en) * 2012-01-06 2013-06-18 Hamilton Sundstrand Corporation Magnetically coupled contra-rotating propulsion stages
DK201270179A (en) * 2012-04-11 2013-10-11 Envision Energy Denmark Aps Wind turbine with improved cooling
GB201207754D0 (en) * 2012-05-03 2012-06-13 Rolls Royce Plc Electro-magnetic coupling system
JP2015028333A (ja) * 2013-07-30 2015-02-12 畑中 武史 航空機用ネットゼロエネルギー推進方法及びネットゼロエネルギー航空機
US11162424B2 (en) * 2013-10-11 2021-11-02 Reaction Engines Ltd Heat exchangers
EP3074605B1 (de) * 2013-11-26 2018-12-05 United Technologies Corporation Gebläseschaufel mit segmentierter ventilatorschaufelabdeckung
US9325224B2 (en) * 2013-12-28 2016-04-26 Google Inc. Electrically-isolated and liquid-cooled rotor and stator assemblies
GB201406952D0 (en) 2014-04-17 2014-06-04 Rolls Royce Plc Open rotor propulsion engine
US11391298B2 (en) * 2015-10-07 2022-07-19 General Electric Company Engine having variable pitch outlet guide vanes
CN205203403U (zh) * 2015-10-30 2016-05-04 湖北易瓦特科技股份有限公司 动力源
US10830097B2 (en) * 2016-02-04 2020-11-10 General Electric Company Engine casing with internal coolant flow patterns
FR3048727B1 (fr) 2016-03-14 2018-03-02 Safran Aircraft Engines Conduit d'entree d'air pour une turbomachine d'aeronef
US10826343B2 (en) * 2016-11-17 2020-11-03 General Electric Company High speed electric machine with radially supported rotor magnets
US10218232B2 (en) * 2016-11-17 2019-02-26 General Electric Company High speed electric machine

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63289229A (ja) * 1987-05-06 1988-11-25 エムテーウー・モートレン‐ウント・ツルビーネン‐ウニオン・ミュンヘン・ゲーエムベーハー プロップ・ファン・ターボ駆動装置
US20130265848A1 (en) * 2010-06-01 2013-10-10 Esg Mbh Duct having flow conducting surfaces
US9701399B1 (en) * 2013-03-18 2017-07-11 Techdyne Llc Parasitic drag induced boundary layer reduction system and method
WO2015004370A1 (fr) * 2013-07-12 2015-01-15 Hutchinson Dispositif de sustentation à soufflante(s) axiale(s), et aerodyne equipé d'un tel dispositif
EP2913269A1 (de) * 2014-02-28 2015-09-02 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Drehflügler mit mindestens einem Hauptrotor und mindestens einem Rotor zum Drehmomentausgleich

Also Published As

Publication number Publication date
EP3765361A4 (de) 2021-12-08
JP2023159233A (ja) 2023-10-31
US20190329858A1 (en) 2019-10-31
WO2020033010A3 (en) 2020-05-22
US11312471B2 (en) 2022-04-26
US11161589B2 (en) 2021-11-02
JP7333144B2 (ja) 2023-08-24
WO2020033010A2 (en) 2020-02-13
US20220169362A1 (en) 2022-06-02
EP3765361A2 (de) 2021-01-20
US20190329859A1 (en) 2019-10-31
JP2021515726A (ja) 2021-06-24
US11912393B2 (en) 2024-02-27

Similar Documents

Publication Publication Date Title
JP7333144B2 (ja) 航空機抗力低減システム及び内部冷却電気モータ・システム並びにこれらを使用する航空機
CN110035954B (zh) 用于私人飞机的通风旋翼安装臂架
JP6322647B2 (ja) 垂直離着陸機
CN107458599B (zh) 电分布式推进反扭矩冗余电力及控制系统
US6808140B2 (en) Vertical take-off and landing vehicles
US8733690B2 (en) Lightweight vertical take-off and landing aircraft and flight control paradigm using thrust differentials
US5242132A (en) Multi-hulled aircraft/boat
EP3584162B1 (de) Propulsoren und verfahren zur führung eines fluidstroms in einem propulsor
CA2984534C (en) Engine cooling systems for aircraft
JP7478667B2 (ja) 個人用垂直離着陸飛行装置
US10464667B2 (en) Oblique rotor-wing aircraft
CN114026023A (zh) 垂直起降式飞行器和相关控制方法
US20220258858A1 (en) Rotary wing aircraft with a shrouded tail propeller
US20230312122A1 (en) Cooling system for aircraft components
KR20050016643A (ko) 덕트형 공기 동력 장치

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination